I am in validation task for Airfoil NASA 0012 with Angle 10 deg nose up with fluent . but Cd is lower than Experimental , why?

Hey i am in validation task for Airfoil NASA 0012 with Angle 10 deg nose up with fluent the given data:- cord = 0.1524 m span = 0.19 turbulence factor = 1.38 according to sandia80-2114 paper the...

26 September 2018 6,558 19 View